Carbon fiber reinforced plastics in aircraft construction

By Constantinos Soutis. 2005

826 citations recorded by the source corpus.

Subfields: Control and Systems Engineering, Mechanics of Materials

View Paper: https://www.semanticscholar.org/paper/79f616be16bdbe18992377bf82a64fb869493565

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Control and Systems Engineering

1. R. Pethrick
2. Ian Sinclair
3. S. Spearing
4. Tilo Baumbach
5. Lukas Helfen
6. Zhen Li
7. Thomas Blumensath
8. D. Bull

In Mechanics of Materials

1. Ian Sinclair
2. R. Pethrick
3. P. Moreira
4. S. Spearing
5. Tilo Baumbach
6. E. Ramon
7. Lukas Helfen
8. S. Agrawal

Citations in the corpus

• A comparison of multi-scale 3D X-ray tomographic inspection techniques for assessing carbon fibre composite impact damage (2013, methodology): “Tomographic imaging using both laboratory sources and synchrotron radiation (SR) was performed to achieve a multi-scale damage assessment of carbon fibre composites subjected to impact damage, allowing various internal damage modes to be studied in three-dimensions.”
• Successes and challenges in non-destructive testing of aircraft composite structures (2020, background): “required, leading to improved structural weight, more aerodynamically efficient structural configurations and ultimately higher fuel efficiency.(3,5) The latter is crucial as in 2009, the International Civil Aviation Organization (ICAO) declared a cap on CO2 emissions, to provide carbon–neutral grow”
• Metal additive manufacturing in the commercial aviation industry: A review (2019, background): “Moreover, the increasing use of Carbon Fiber Reinforced Polymer (CFRP) materials in aerospace is driving the interest in Titanium alloys [114, 115].”
• A Review of the Radio Frequency Non-destructive Testing for Carbon-fibre Composites (2016, background): “Carbon-fibre reinforced plastics composites (CFRP) have been widely used in aerospace, shipping and automotive structural applications, due to their superior stiffness and strength characteristics, fatigue and corrosion resistance [1].”
• Design and ageing of adhesives for structural adhesive bonding – A review (2015, background): “A weak fibre–matrix interface can lead to a low stiffness and strength but high resistance to fracture, whereas a strong interface produces high stiffness and strength but often a low resistance to fracture.(11) The failure behaviour depends not only on inherent heterogeneity and anisotropy, but als”